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CN203742311U - Wing locking device of wing opening type box van - Google Patents

Wing locking device of wing opening type box van Download PDF

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Publication number
CN203742311U
CN203742311U CN201420082237.4U CN201420082237U CN203742311U CN 203742311 U CN203742311 U CN 203742311U CN 201420082237 U CN201420082237 U CN 201420082237U CN 203742311 U CN203742311 U CN 203742311U
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CN
China
Prior art keywords
wing
locking device
opening type
type box
locking
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Expired - Fee Related
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CN201420082237.4U
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Chinese (zh)
Inventor
黄国浩
朱芒
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China International Marine Containers Group Co Ltd
CIMC Vehicles Group Co Ltd
Shanghai CIMC Special Vehicles Co Ltd
Original Assignee
China International Marine Containers Group Co Ltd
CIMC Vehicles Group Co Ltd
Shanghai CIMC Special Vehicles Co Ltd
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Application filed by China International Marine Containers Group Co Ltd, CIMC Vehicles Group Co Ltd, Shanghai CIMC Special Vehicles Co Ltd filed Critical China International Marine Containers Group Co Ltd
Priority to CN201420082237.4U priority Critical patent/CN203742311U/en
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Publication of CN203742311U publication Critical patent/CN203742311U/en
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Expired - Fee Related legal-status Critical Current

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Abstract

本实用新型提出一种翼开启厢式车及其翼翅锁紧装置,翼翅锁紧装置用于将翼开启厢式车的两侧的翼翅锁固于车体,翼翅锁紧装置包括第一锁紧机构,第一锁紧机构包括:操作件;两个第一连接件,每一个第一连接件的一端与操作件铰接于第二铰接点;两个第一锁钩,分别与两个第一连接件的另一端铰接于第三铰接点;第一导向槽,设置在翼开启厢式车的两侧,并导引两个第一锁钩滑动;所述操作件能够被操作以使两个第一连接件带动两个第一锁钩沿着第一导向槽滑动,以与翼翅的锁舌相互锁合或相互脱离。本实用新型提出的翼翅锁紧装置和翼开启厢式车,通过操作杆推拉,实现翼翅的锁紧和松开操作方便。此翼翅锁紧装置操作简单,安装方便,通用性强,可靠性高。

The utility model proposes a wing-opening van and its wing locking device. The wing locking device is used to lock the wings on both sides of the wing-opening van to the vehicle body. The wing locking device includes The first locking mechanism, the first locking mechanism includes: an operating part; two first connecting parts, one end of each first connecting part is hinged to the operating part at a second hinge point; two first locking hooks, respectively The other ends of the two first connecting parts are hinged at the third hinge point; the first guide slots are arranged on both sides of the wing-opening van and guide the sliding of the two first locking hooks; the operating parts can be operated The two first connecting parts drive the two first locking hooks to slide along the first guide groove, so as to lock or disengage from the locking tongues of the wings. The wing-fin locking device and the wing-opening van provided by the utility model realize the locking and loosening of the wings by pushing and pulling the operating lever, which is convenient to operate. The wing locking device is simple in operation, convenient in installation, strong in versatility and high in reliability.

Description

翼开启厢式车的翼翅锁紧装置Wing locking device for wing-opening van

技术领域 technical field

本实用新型涉及一种翼开启厢式车,特别涉及一种翼开启厢式车及其翼翅锁紧装置。  The utility model relates to a wing-opening van, in particular to a wing-opening van and a wing locking device thereof. the

背景技术 Background technique

图1为现有的翼开启厢式车的翼翅锁紧装置的剖视图。如图1所示,目前翼开启厢式车的翼翅锁紧装置包括支撑板11、被动转臂12、扭臂13、锁钩14、锁舌15、外侧支撑16、翼钩17和操纵杆18。  Fig. 1 is a cross-sectional view of a wing locking device of a conventional wing-opening van. As shown in Figure 1, the wing locking device of the wing-opening van currently includes a support plate 11, a passive rotating arm 12, a torsion arm 13, a locking hook 14, a locking tongue 15, an outer support 16, a wing hook 17 and an operating lever. 18. the

图1中现有的翼翅锁紧装置的工作原理如下:支撑板11上铰接有操纵杆18,通过操纵杆18旋转带动被动转臂12,带动扭臂13旋转,外侧支撑16旋转,锁钩14与锁舌15扣在一起,从而对翼翅17进行锁紧。  The working principle of the existing wing locking device in Fig. 1 is as follows: a joystick 18 is hinged on the support plate 11, and the rotation of the joystick 18 drives the passive arm 12, drives the torsion arm 13 to rotate, the outer support 16 rotates, and the locking hook 14 is buckled together with the deadbolt 15, thereby locking the wings 17. the

现有的翼翅锁紧装置机构的结构复杂、加工精度要求高;由于制造和加工误差,很可能造成锁紧机构无法正常工作,为开锁和锁紧的操作不方便。  The structure of the existing wing locking device mechanism is complex and requires high processing precision; due to manufacturing and processing errors, the locking mechanism may not work normally, and the operation of unlocking and locking is inconvenient. the

发明内容 Contents of the invention

本实用新型的目的是提出一种翼开启厢式车及其翼翅锁紧装置,以解决现有技术存在的问题。  The purpose of the utility model is to propose a wing-opening van and its wing-wing locking device to solve the problems in the prior art. the

为实现上述目的,本实用新型一实施例提出一种翼开启厢式车的翼翅锁紧装置,用于将所述翼开启厢式车的两侧的翼翅锁固于车体,所述翼翅锁紧装置包括第一锁紧机构,所述第一锁紧机构包括:  In order to achieve the above purpose, an embodiment of the present utility model proposes a wing locking device of a wing-opening van, which is used to lock the wings on both sides of the wing-opening van to the vehicle body. The wing locking device includes a first locking mechanism, and the first locking mechanism includes:

操作件;  operating parts;

两个第一连接件,每一个所述第一连接件的一端与所述操作件铰接于第二铰接点;  Two first connecting parts, one end of each of the first connecting parts is hinged to the operating part at a second hinge point;

两个第一锁钩,分别与所述两个第一连接件的另一端铰接于第三铰接点;  The two first lock hooks are respectively hinged to the other ends of the two first connectors at the third hinge point;

第一导向槽,设置在所述翼开启厢式车的两侧,并导引所述两个第一锁钩滑动;  The first guide groove is arranged on both sides of the wing-opening van, and guides the sliding of the two first lock hooks;

所述操作件能够被操作以使所述两个第一连接件带动所述两个第一锁钩沿着所述第一导向槽滑动,以与所述翼翅的锁舌相互锁合或相互脱离。  The operating member can be operated so that the two first connecting members drive the two first locking hooks to slide along the first guide groove to lock or lock the locking tongue of the wing. break away. the

在本实用新型翼翅锁紧装置的一实施例中,所述操作件在所述第一锁钩与所述翼翅的所述锁舌相互锁合后被固定在所述车体。  In an embodiment of the wing locking device of the present invention, the operating member is fixed on the vehicle body after the first locking hook and the locking tongue of the wing are locked with each other. the

在本实用新型翼翅锁紧装置的一实施例中,所述操作件包括操作杆和传动杆,所述操作杆与所述传动杆的一端连接,所述传动杆的另一端与所述两个第一连接件铰接于所述第二铰接点。  In one embodiment of the wing locking device of the present invention, the operating member includes an operating rod and a transmission rod, the operating rod is connected to one end of the transmission rod, and the other end of the transmission rod is connected to the two A first connecting piece is hinged at the second hinge point. the

在本实用新型翼翅锁紧装置的一实施例中,所述翼翅锁紧装置还包括延伸锁紧机构,所述延伸锁紧机构与所述第一锁紧机构连接,所述延伸锁紧机构包括:  In an embodiment of the wing locking device of the present invention, the wing locking device further includes an extension locking mechanism, the extension locking mechanism is connected with the first locking mechanism, and the extension locking mechanism Agencies include:

联动板;  linkage plate;

两个第二连接件,所述两个第二连接件的一端铰接所述联动板的另一端于第四铰接点;以及  Two second connectors, one end of the two second connectors hinges the other end of the linkage plate at the fourth hinge point; and

两个第二锁钩,分别与所述两个第二连接件的另一端铰接于第五铰接点;  Two second locking hooks are respectively hinged to the other ends of the two second connectors at the fifth hinge point;

第二导向槽,设置在所述翼开启厢式车的两侧,并导引所述两个第二锁钩滑动;  The second guide groove is arranged on both sides of the wing-opening van, and guides the sliding of the two second locking hooks;

所述联动板能够被所述操作件驱动以使所述两个第二连接件带动所述两个第二锁钩沿着所述第二导向槽滑动,以与所述翼翅的锁舌相互锁合或相互脱离。  The linkage plate can be driven by the operating part so that the two second connecting parts drive the two second locking hooks to slide along the second guide groove to interact with the locking tongue of the wing. locked or disengaged from each other. the

在本实用新型翼翅锁紧装置的一实施例中,所述联动板的一端与所述传动杆铰接于所述第二铰接点。  In an embodiment of the wing locking device of the present invention, one end of the linkage plate is hinged to the transmission rod at the second hinge point. the

在本实用新型翼翅锁紧装置的一实施例中,延伸锁紧机构为两组,其中一组所述延伸锁紧机构通过其联动板铰接于所述第二铰接点,另一组所述延伸锁紧机构通过其联动板铰接于所述第四铰接点。  In one embodiment of the wing locking device of the present utility model, the extension locking mechanism is divided into two groups, wherein one group of the extension locking mechanism is hinged to the second hinge point through its linkage plate, and the other group is the The extension locking mechanism is hinged to the fourth hinge point through its linkage plate. the

在本实用新型翼翅锁紧装置的一实施例中,所述第一锁紧机构的所述第一连接件和所述延伸锁紧机构的所述第二连接件相互平行设置。  In an embodiment of the wing locking device of the present invention, the first connecting part of the first locking mechanism and the second connecting part of the extending locking mechanism are arranged parallel to each other. the

在本实用新型翼翅锁紧装置的一实施例中,所述操作杆与所述传动杆的一端铰接于第一铰接点。  In an embodiment of the wing locking device of the present invention, one end of the operating rod and the transmission rod is hinged at a first hinge point. the

本实用新型还提出一种翼开启厢式车,包括车体和翼翅,所述翼翅设置在所述车体的两侧,所述翼翅包括锁舌,所述翼开启厢式车还包括翼翅锁紧 装置,所述翼翅锁紧装置为上述的翼翅锁紧装置。  The utility model also proposes a wing-opening van, which includes a car body and wings. The wings are arranged on both sides of the car body. The wings include a lock tongue. Including wing locking device, described wing locking device is above-mentioned wing locking device. the

在本实用新型翼开启厢式车的一实施例中,所述车体上具有锁杆手柄,所述操作件在所述第一锁钩与所述翼翅与所述锁舌相互锁合后被所述锁杆手柄固定在所述车体。  In an embodiment of the wing-opening van of the present invention, the vehicle body is provided with a lock lever handle, and the operating member is locked after the first lock hook, the wing and the lock tongue are locked together. It is fixed on the car body by the lock bar handle. the

本实用新型提出一种翼翅锁紧装置和翼开启厢式车,通过操作杆推拉,实现翼翅的锁紧和松开操作方便。此翼翅锁紧装置和翼开启厢式车操作简单,安装方便,通用性强,可靠性高。  The utility model provides a wing-wing locking device and a wing-opening van. The locking and loosening of the wings can be easily operated by pushing and pulling an operating rod. The wing-wing locking device and the wing-opening van have simple operation, convenient installation, strong versatility and high reliability. the

附图说明 Description of drawings

图1为现有翼开启厢式车的翼翅锁紧装置在锁紧状态下的剖视图;  Fig. 1 is the cross-sectional view of the wing locking device of the existing wing-opening van in the locked state;

图2为本实用新型一实施例的翼开启厢式车的翼翅锁紧装置在翼翅开启状态下的仰视图;  Fig. 2 is a bottom view of the wing locking device of the wing-opening van of an embodiment of the utility model in the wing-open state;

图3为本实用新型一实施例的翼翅锁紧装置在翼翅锁紧状态下的俯视图;  Fig. 3 is a top view of the wing locking device of an embodiment of the present invention under the wing locking state;

图4为本实用新型一实施例的翼翅锁紧装置在翼翅开启状态下的剖视图;  Fig. 4 is a cross-sectional view of the wing locking device of an embodiment of the present invention when the wings are opened;

图5为本实用新型一实施例的翼翅锁紧装置在翼翅锁紧状态下的剖视图;  Fig. 5 is a sectional view of the wing locking device of an embodiment of the present invention under the wing locking state;

图6为本实用新型一实施例的翼翅锁紧装置的另一实施例的示意图。  Fig. 6 is a schematic diagram of another embodiment of the wing locking device of an embodiment of the present invention. the

图7为本实用新型一实施例的翼翅锁紧装置在翼翅锁紧状态下的后视图;  Fig. 7 is a rear view of the wing locking device of an embodiment of the present invention under the wing locking state;

图8为本实用新型一实施例的翼翅锁紧装置在翼翅锁紧状态下的剖视图。  Fig. 8 is a cross-sectional view of the wing locking device in a wing locking state according to an embodiment of the present invention. the

具体实施方式 Detailed ways

本实用新型实施例提出一种翼开启厢式车和翼翅锁紧装置,翼开启厢式车包括车体、翼翅10和翼翅锁紧装置,翼翅锁紧装置设置在车体的底部。  The embodiment of the utility model proposes a wing-opening van and a wing-wing locking device. The wing-opening van includes a car body, wings 10 and a wing-wing locking device, and the wing-wing locking device is arranged at the bottom of the car body . the

图2为本实用新型一实施例的翼开启厢式车的翼翅锁紧装置在翼翅开启状态下的仰视图,图3为本实用新型一实施例的翼翅锁紧装置在翼翅锁紧状态下的俯视图;图4和图5分别为对应图2和图3的翼翅开启和锁紧状态下 的剖视图。  Fig. 2 is a bottom view of the wing locking device of a wing-opening van according to an embodiment of the utility model in the wing-open state, and Fig. 3 is a bottom view of the wing locking device of an embodiment of the utility model under the wing lock Top view under tight state; Fig. 4 and Fig. 5 are the cross-sectional views corresponding to Fig. 2 and Fig. 3 under the open and locked state of the wings respectively. the

如图2和图3所示,本实用新型一实施例的翼翅锁紧装置包括第一锁紧机构,所述第一锁紧机构包括操作件20、两个第一连接件23、两个第一锁钩24和第一导向槽26。操作件20包括操作杆21和传动杆22。再如图4和图5所示,翼翅10上具有锁舌101,翼翅锁紧装置的两个第一锁钩24能够锁固在锁舌101上,或者与锁舌101相互脱离释放。当翼翅锁紧装置的第一锁钩24脱离翼翅10的锁舌101(如图4),则翼翅10相对于车体(图未示)解锁;当第一锁钩24与翼翅10的锁舌101相互接触(如图5),则翼翅10被锁固于车体。  As shown in Fig. 2 and Fig. 3, the wing locking device according to an embodiment of the present invention includes a first locking mechanism, and the first locking mechanism includes an operating part 20, two first connecting parts 23, two The first lock hook 24 and the first guide groove 26 . The operating member 20 includes an operating rod 21 and a transmission rod 22 . As shown in FIGS. 4 and 5 , the wing 10 has a locking tongue 101 , and the two first locking hooks 24 of the wing locking device can be locked on the locking tongue 101 , or can be separated from the locking tongue 101 for release. When the first locking hook 24 of the wing locking device breaks away from the locking tongue 101 of the wing 10 (as shown in Figure 4), the wing 10 is unlocked relative to the vehicle body (not shown); when the first locking hook 24 is connected to the wing The dead bolts 101 of 10 are in contact with each other (as shown in FIG. 5 ), and the wings 10 are locked to the vehicle body. the

如图2和图3的所示,翼翅锁紧装置的操作杆21和传动杆22在第一铰接点R1铰接;传动杆22和第一连接件23在第二铰接点R2铰接;两个第一连接件23分别与两侧的第一锁钩24在第三铰接点R3铰接。第一锁钩24设置于第一导向槽26中,并能够沿着第一导向槽26的导向方向即图2中所示的A方向及其反方向水平滑动。操作杆21可以被沿着图2中所示的B方向及其反方向拉动或推动,从而带动传动杆22向图2所示的B方向及其反方向运动。  As shown in Figure 2 and Figure 3, the operating rod 21 and the transmission rod 22 of the wing locking device are hinged at the first hinge point R1; the transmission rod 22 and the first connecting member 23 are hinged at the second hinge point R2; The first connecting member 23 is respectively hinged with the first locking hooks 24 on both sides at the third hinge point R3. The first locking hook 24 is disposed in the first guiding groove 26 and can slide horizontally along the guiding direction of the first guiding groove 26 , namely the direction A shown in FIG. 2 and its opposite direction. The operating rod 21 can be pulled or pushed along the direction B shown in FIG. 2 and its opposite direction, thereby driving the transmission rod 22 to move in the direction B shown in FIG. 2 and its opposite direction. the

结合图2和图3所示,当使用者沿着图2中的B方向拉动操作杆21,由传动杆22带动第一连接件23向B方向移动,两个第一连接件23之间的夹角由180°减小,两个第三铰接点R3之间的直线距离减小,带动两个第一锁钩24分别向车体的内侧滑动;再结合图4和图5所示,每一个第一锁钩24由图4的与翼翅10的锁舌101脱离的位置移动至图5的与翼翅10的锁舌101结合的位置,从而将翼翅10锁固在车体上。  As shown in FIG. 2 and FIG. 3 , when the user pulls the operating lever 21 along the direction B in FIG. The included angle is reduced from 180°, and the straight-line distance between the two third hinge points R3 is reduced, driving the two first locking hooks 24 to slide towards the inner side of the car body respectively; A first locking hook 24 is moved from the position disengaged from the locking tongue 101 of the wing 10 in FIG. 4 to the position combined with the locking tongue 101 of the wing 10 in FIG. 5 , thereby locking the wing 10 on the vehicle body. the

在本实施例中,为了增加翼翅锁紧装置的稳固性,还增设有延伸锁紧机构。延伸锁紧机构包括联动板25、两个第二连接件23’、两个第二锁钩24’、第二导向槽26’。联动板25’的一端与传动杆22在第二铰接点R2铰接,另一端铰接两个第二连接件23’,且铰接点为第四铰接点R4。两个第二连接件23’与第一连接件23相互平行,两个第二连接件23’的另一端分别铰接第二锁钩24’,并且铰接点为第五铰接点R5,第二锁钩24’设置在第二导向槽26’中,以通过联动板25的拉动在第二导向槽26’中滑动。  In this embodiment, in order to increase the stability of the wing locking device, an extension locking mechanism is additionally provided. The extension locking mechanism includes a linkage plate 25, two second connecting pieces 23', two second lock hooks 24', and a second guide groove 26'. One end of the linkage plate 25' is hinged with the transmission rod 22 at the second hinge point R2, and the other end is hinged with two second connecting parts 23', and the hinge point is the fourth hinge point R4. The two second connecting parts 23' are parallel to the first connecting part 23, and the other ends of the two second connecting parts 23' are respectively hinged to the second lock hook 24', and the hinge point is the fifth hinge point R5, the second lock The hook 24 ′ is disposed in the second guide groove 26 ′ to slide in the second guide groove 26 ′ by being pulled by the linkage plate 25 . the

结合图2和图3所示,在翼翅锁紧装置包括第一锁紧机构和延伸锁紧机 构的情况下,当使用者沿着图2中的B方向拉动操作杆21,由传动杆22带动第一连接件23向B方向移动,并由与传动杆22铰接的联动板25带动第二连接件23’向B方向移动,两个第一连接件23之间的夹角由180°逐渐减小,两个第二连接件23’之间的夹角由180°逐渐减小;两个第三铰接点R3之间的直线距离减小,两个第五铰接点R5之间的直线距离也减小;带动两个第一锁钩24和两个第二锁钩24’分别向内滑动;再结合图4和图5所示,每一个锁钩24和第二锁钩24’由图4的与翼翅10的锁舌101脱离的位置移动至图5的与翼翅10的锁舌101结合的位置,从而将翼翅10锁固在车体上。  As shown in Figure 2 and Figure 3, in the case where the wing locking device includes a first locking mechanism and an extension locking mechanism, when the user pulls the operating lever 21 along the direction B in Figure 2, the transmission lever 22 drives the first connecting piece 23 to move in the B direction, and the linkage plate 25 hinged with the transmission rod 22 drives the second connecting piece 23' to move in the B direction, and the angle between the two first connecting pieces 23 changes from 180° gradually decreases, the angle between the two second connectors 23' gradually decreases from 180°; the straight-line distance between the two third hinge points R3 decreases, and the straight line between the two fifth hinge points R5 The distance is also reduced; the two first lock hooks 24 and the two second lock hooks 24' are driven to slide inward respectively; and as shown in Figure 4 and Figure 5, each lock hook 24 and the second lock hook 24' are formed by The position disengaged from the locking tongue 101 of the wing 10 in FIG. 4 is moved to the position combined with the locking tongue 101 of the wing 10 in FIG. 5 , thereby locking the wing 10 on the vehicle body. the

图6为本实用新型一实施例的翼翅锁紧装置的另一实施例的示意图。在本实施例中,可以根据车体的长度增加延伸锁紧机构来实现锁紧。在本实施例中延伸锁紧机构为两组,其中一组延伸锁紧机构通过其联动板25铰接于第二铰接点R2,另一组延伸锁紧机构通过其联动板25铰接于第四铰接点R4。虽然本实施例以两组延伸锁紧机构为例进行说明,然而本领域普通技术人员应当可以理解,还可以设置更多组的延伸锁紧机构,使本实用新型的翼翅锁紧装置的锁紧更加稳固。  Fig. 6 is a schematic diagram of another embodiment of the wing locking device of an embodiment of the present invention. In this embodiment, locking can be realized by adding and extending the locking mechanism according to the length of the vehicle body. In this embodiment, there are two sets of extension locking mechanisms, one set of extension locking mechanisms is hinged to the second hinge point R2 through its linkage plate 25, and the other set of extension locking mechanisms is hinged to the fourth hinge point through its linkage plate 25. Point R4. Although the present embodiment takes two sets of extension locking mechanisms as an example, those skilled in the art should understand that more sets of extension locking mechanisms can be provided to make the lock of the wing locking device of the present utility model Tighter and more stable. the

图7为本实用新型一实施例的翼翅锁紧装置在翼翅锁紧状态下的后视图;图8为图7中锁紧状态下的局部剖视图。如图7和图8所示,在将翼翅10锁紧之后,将操作杆21绕着第一铰接点R1旋转,使操作杆21枢转至平行于车体后厢门30的位置,并位于设置在后厢门30上的另外的锁固装置的锁杆手柄40的内侧;将锁杆手柄40固定,从而将操作杆21锁固在后厢门30上,就可以避免翼翅10的开启。  Fig. 7 is a rear view of the wing locking device according to an embodiment of the present invention in the wing locking state; Fig. 8 is a partial cross-sectional view in Fig. 7 in the locking state. As shown in FIGS. 7 and 8 , after the wing 10 is locked, the operating lever 21 is rotated around the first hinge point R1, so that the operating lever 21 is pivoted to a position parallel to the rear compartment door 30 of the vehicle body, and Be positioned at the inner side of the lock lever handle 40 of the other locking device that is arranged on the tailgate 30; Fix the lock lever handle 40, thereby operating rod 21 is locked on the tailgate 30, just can avoid wing 10. open. the

当需要开启翼翅10时,打开锁杆手柄40,将操作杆21枢转至图3所示的位置,将操作杆21水平向内推,操作杆21带动传动杆22向前(即B方向的反方向)运动,传动杆22带动第一连接件23、第二连接件23’和联动板25运动,两边连接件23之间的夹角变大,带动两侧锁钩24向车外移动,与两侧翼翅10脱离,即可打开翼翅10。  When it is necessary to open the wing 10, open the lock lever handle 40, pivot the operating lever 21 to the position shown in Figure 3, push the operating lever 21 horizontally inward, and the operating lever 21 drives the transmission lever 22 forward (that is, the direction B The opposite direction) movement, the transmission rod 22 drives the first connecting part 23, the second connecting part 23' and the linkage plate 25 to move, the angle between the connecting parts 23 on both sides becomes larger, and drives the locking hooks 24 on both sides to move out of the vehicle , separated from the wings 10 on both sides, the wings 10 can be opened. the

本实用新型还提出一种翼开启厢式车,包括车体和翼翅10,并包括上述的翼翅锁紧装置。其中,翼翅锁紧装置是位于车体的下方,并且翼翅锁紧装置的操作杆21能够在锁固翼翅10之后固定于车体的后厢门30的锁杆手柄40处。  The utility model also proposes a wing-opening van, which includes a vehicle body and wings 10, and includes the above-mentioned wing locking device. Wherein, the wing locking device is located below the vehicle body, and the operating lever 21 of the wing locking device can be fixed to the lock lever handle 40 of the rear compartment door 30 of the vehicle body after locking the wing 10 . the

由上述描述可知,本实用新型提出一种翼翅锁紧装置和翼开启厢式车,通过操作杆21推拉,实现翼翅的锁紧和松开操作方便;并且可以根据车体的长度增加联动板和锁钩来实现锁紧,此翼翅锁紧装置和翼开启厢式车操作简单,安装方便,通用性强,可靠性高。  It can be seen from the above description that the utility model proposes a wing locking device and a wing opening van, and the locking and loosening of the wings can be realized by pushing and pulling the operating rod 21; and the linkage can be increased according to the length of the car body. The locking device and the wing-opening van are easy to operate, easy to install, strong in versatility and high in reliability. the

虽然已参照几个典型实施例描述了本实用新型,但应当理解,所用的术语是说明和示例性、而非限制性的术语。由于本实用新型能够以多种形式具体实施而不脱离本实用新型的精神或实质,所以应当理解,上述实施例不限于任何前述的细节,而应在所附权利要求所限定的精神和范围内广泛地解释,因此落入权利要求或其等效范围内的全部变化和改型都应为所附权利要求所涵盖。  While the invention has been described with reference to a few exemplary embodiments, it is to be understood that the words which have been used are words of description and illustration, rather than of limitation. Since the present invention can be embodied in various forms without departing from the spirit or essence of the present invention, it should be understood that the above-described embodiments are not limited to any of the foregoing details, but should be within the spirit and scope of the appended claims. Broadly interpreted, all changes and modifications that come within the scope of the claims or their equivalents are therefore intended to be covered by the appended claims. the

Claims (10)

1. a wing locking device for wing opening type box van, for the wing of the both sides of described wing opening type box van (10) is locked in to car body, is characterized in that, described wing locking device comprises the first retaining mechanism, and described the first retaining mechanism comprises:
Operating parts (20);
Two the first connectors (23), described in each, one end of the first connector (23) and described operating parts (20) are articulated with the second pin joint (R2);
Two the first latch hooks (24), are articulated with the 3rd pin joint (R3) with the other end of described two the first connectors (23) respectively;
The first gathering sill (26), is arranged on the both sides of described wing opening type box van, and guides described two the first latch hooks (24) and slide;
Described operating parts (20) can be operated to described two the first connectors (23) and drive described two the first latch hooks (24) to slide along described the first gathering sill (26), to be mutually locked with the dead bolt (101) of described wing (10) or mutually to depart from.
2. the wing locking device of wing opening type box van as claimed in claim 1, it is characterized in that, described operating parts (20) is fixed on described car body after described the first latch hook (24) and the described dead bolt (101) of described wing (10) are mutually locked.
3. the wing locking device of wing opening type box van as claimed in claim 1, it is characterized in that, described operating parts (20) comprises action bars (21) and drive link (22), described action bars (21) is connected with one end of described drive link (22), and the other end of described drive link (22) and described two the first connectors (23) are articulated with described the second pin joint (R2).
4. the wing locking device of wing opening type box van as claimed in claim 3, is characterized in that, described wing locking device also comprises extension retaining mechanism, and described extension retaining mechanism is connected with described the first retaining mechanism, and described extension retaining mechanism comprises:
Linkage board (25);
Two the second connectors (23 '), the other end of the hinged described linkage board in one end (25) of described two the second connectors (23 ') is in the 4th pin joint (R4); And
Two the second latch hooks (24 '), are articulated with the 5th pin joint (R5) with the other end of described two the second connectors (23 ') respectively;
The second gathering sill (26 '), is arranged on the both sides of described wing opening type box van, and guides described two the second latch hooks (24 ') and slide;
Described linkage board (25) can be driven by described operating parts (20) so that described two the second connectors (23 ') drive described two the second latch hooks (24 ') to slide along described the second gathering sill (26 '), to be mutually locked with the dead bolt (101) of described wing (10) or mutually to depart from.
5. the wing locking device of wing opening type box van as claimed in claim 4, is characterized in that, one end of described linkage board (25) and described drive link (22) are articulated with described the second pin joint (R2).
6. the wing locking device of wing opening type box van as claimed in claim 4, it is characterized in that, described wing locking device comprises that two groups are extended retaining mechanism, wherein described in one group, extend retaining mechanism and be articulated with described the second pin joint (R2) by its linkage board (25), another is organized described extension retaining mechanism and is articulated with described the 4th pin joint (R4) by its linkage board (25).
7. the wing locking device of wing opening type box van as claimed in claim 6, it is characterized in that, described second connector (23 ') of described first connector (23) of described the first retaining mechanism and described extension retaining mechanism is arranged in parallel.
8. the wing locking device of wing opening type box van as claimed in claim 3, is characterized in that, described action bars (21) is articulated with the first pin joint (R1) with one end of described drive link (22).
9. a wing opening type box van, comprise car body and wing (10), described wing (10) is arranged on the both sides of described car body, described wing (10) comprises dead bolt (101), it is characterized in that, described wing opening type box van also comprises wing locking device, and described wing locking device is the wing locking device as described in any one in claim 1-8.
10. wing opening type box van as claimed in claim 9, it is characterized in that, on described car body, have lock bar handle (40), described operating parts (20) is fixed on described car body by described lock bar handle (40) after described the first latch hook (24) and the described dead bolt (101) of described wing (10) are mutually locked.
CN201420082237.4U 2014-02-25 2014-02-25 Wing locking device of wing opening type box van Expired - Fee Related CN203742311U (en)

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Application Number Priority Date Filing Date Title
CN201420082237.4U CN203742311U (en) 2014-02-25 2014-02-25 Wing locking device of wing opening type box van

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108301706A (en) * 2018-02-24 2018-07-20 上海宜社实业有限公司 A kind of fuel tank cap lock and its intelligent oil tank cover and antitheft oil system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108301706A (en) * 2018-02-24 2018-07-20 上海宜社实业有限公司 A kind of fuel tank cap lock and its intelligent oil tank cover and antitheft oil system

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